CN106624330B - A kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board - Google Patents
A kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board Download PDFInfo
- Publication number
- CN106624330B CN106624330B CN201710052452.8A CN201710052452A CN106624330B CN 106624330 B CN106624330 B CN 106624330B CN 201710052452 A CN201710052452 A CN 201710052452A CN 106624330 B CN106624330 B CN 106624330B
- Authority
- CN
- China
- Prior art keywords
- copper
- stainless steel
- magnesium alloy
- plate
- explosive
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/06—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of high energy impulses, e.g. magnetic energy
- B23K20/08—Explosive welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/24—Preliminary treatment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/18—Dissimilar materials
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
A kind of explosive welding processing method of stainless steel copper magnesium alloy composite plate, belongs to composite plate preparing technical field, it is characterised in that：The use of stainless steel is cladding, magnesium alloy is base, and sheet copper is transition zone, using expanded ammonium nitrate composite explosives as the explosion energy.The present invention is according on stainless steel and two kinds of material metallurgy of magnesium alloy the characteristics of indissoluble, using copper as transition zone progress explosive welding.Magnesium alloy plate is made annealing treatment before explosive welding, mechanical grinding stainless steel, copper coin, magnesium alloy plate face to be combined, after stainless steel, sheet copper, magnesium alloy combination, on earthen foundation, rubber layer is laid on ground, using expanded ammonium nitrate composite explosives, electric cap is remotely ignited.The present invention is easy to operate, and economical, Surface bond rate 99.8%, 165 ~ 183Mpa of interface bond strength is the feasible method for preparing stainless steel copper magnesium alloy laminated composite plate.
Description
Technical field
The invention belongs to composite plate preparing technical fields, especially relate to the explosion welding method of stainless steel-copper-magnesium composite plate.
Background technology
The deficiencies of intrinsic plastic deformation ability of magnesium alloy is low, surface gap sensibility is strong, corrosion resistance is poor so that magnesium alloy
Application relative to numerous metal materials is quite limited.Improving the corrosive method of Mg alloy surface at present has plating, changes
It learns the methods of plating, thermal spraying to add metal coating for Mg alloy surface, improves the corrosivity of magnesium alloy substrate.Aforesaid operations are multiple
It is miscellaneous, be not suitable for the magnesium alloy plate of manufacture large area, and coating is thin, easy to fall off, coating does not have the mechanical property of magnesium alloy substrate
There is improvement.
Stainless steel is a kind of high-alloy steel that can resist acid, alkali, salt and its solution and the corrosion of some other corrosive medium,
It is cheap, it is one of most widely used metal in industrial production.Stainless steel also has excellent in addition to outstanding corrosion resistance
Mechanical strength, high-temperature oxidation and toughness.Have that plasticity is high, erosion-resisting feature in view of stainless steel, if by magnesium alloy with
Stainless steel combines and laminated composite plate is made, and can not only improve magnesium alloy materials surface corrosion resistance performance, can also improve magnesium alloy
The comprehensive mechanical property of basis material meets the service demand of material.This is the effective way for widening magnesium alloy plate application, tool
There is important Practical significance.
Composite plate manufacture mainly has two methods of explosive welding and rolling, and rolling connection is to equipment precision requirement height, assembly
Complexity, manufacturing cost is high, and during the rolling process, since top and bottom rolls pressure is different, be easy to cause milled sheet discontinuity,
Cause to crack.Explosive welding process is widely used the combination, it can be achieved that various metals bilayer and multilayer, moment forming, bond strength
It is high.Known by magnesium iron binary phase diagraml, magnesium ferro element fusing point differs greatly, and the two solubility is zero, also without intermetallic produce
It gives birth to, therefore is difficult to realize the high strength bond of the two with traditional explosion weld process.Magnesium alloy plasticity is poor, and implements explosion
The difficult point of welding.
Goal of the invention
The purpose of the present invention is the situations for background technology to be utilized by the patent to magnesium alloy materials before welding
Specific explosion weld process realizes indissoluble on metallurgy, the stainless steel and magnesium that fusing point differs greatly using copper coin as transition zone
The connection of alloy is made stainless steel copper magnesium alloy composite plate and magnesium alloy matrix surface corrosion resistance and comprehensive mechanical property can be improved,
The present invention helps to expand the use scope of magnesium alloy plate.
A kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board, it is characterised in that：It is using stainless steel
Cladding, magnesium alloy are base, and sheet copper is transition zone, using expanded ammonium nitrate composite explosives as the explosion energy.
A kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board, includes the following steps：
（1）Select magnesium alloy plate and stainless steel plate as the base material of explosive welding, and to magnesium alloy annealing toughening, annealing temperature
Degree is 300 DEG C, soaking time 120min；
（2）Stainless steel plate interface to be combined, magnesium alloy plate interface to be combined just polish with angle grinder, then used
The sand paper of 600 mesh carries out smart polishing, and surface roughness Ra to be combined is made to be no more than 2 μm；Sheet copper upper and lower surface is beaten with 600 mesh sand paper
Mill makes sheet copper upper and lower surface roughness be no more than 2 μm；
（3）By stainless steel plate, sheet copper and the magnesium alloy board group after polishing to carrying out explosive welding：
Cushion rubber layer is fixed in face to I on the ground；
II places magnesium alloy plate on the buffer layer；
Copper gap column is vertically disposed in above magnesium alloy plate by III, and the spacing between copper gap column is 100mm, copper
Matter gap pillar height degree is（1.5~3）The thickness of × stainless steel plate；
Sheet copper is placed on copper gap column by IV, and sheet copper is parallel with magnesium alloy plate；
Copper gap column is placed above in sheet copper in V, and the spacing between copper gap column is 100mm, copper gap column
Highly it is（1.5~3）The thickness of × stainless steel plate, copper gap column are vertical with sheet copper holding；
VI places stainless steel plate on sheet copper, and stainless steel plate is parallel with magnesium alloy plate；
The VII butter that the uniform smearing thickness of layer surface and edge is 2mm on stainless steel；
VIII bonds brown paper medicine frame and stainless steel plate edge butter；
Uniform thickness is not laid with one layer of explosive above IV butter, and initiation ends explosive thickness is more than explosion ending end explosive thickness；
Explosive layer is seamlessly transitted from initiation ends to explosion end；
Detonator is inserted into explosive layer by X, and the cap length for being inserted into explosive layer is more than the half of initiation ends explosive thickness,
And 5 ~ 8mg hexogen is added in 5 ~ 10mm radius around detonator；
（4）Stainless steel-copper-magnesium alloy three-layer composite board of explosion synthesis is made annealing treatment, with 10 DEG C/sec of speed
It is warming up to 200 DEG C, soaking time 60min of annealing temperature, after heat preservation, composite plate furnace cooling, then in level(l)ing machine colonel
It is flat；
（5）The non-soldering region of composite plate surrounding is cut with plate shearing machine, the remaining butter of stainless steel upper surface side of polishing obtains
Stainless steel-copper-magnesium alloy three-layer composite board；
（6）The Percentage bound of stainless steel-copper-magnesium alloy three-layer composite board is 99.8%, and tensile-sbear strength is 165 ~ 183Mpa, magnesium
It spreads mutually between element and copper, is spread mutually between copper and ferro element；
The copper gap column is that a block length is 20mm, the height of width=copper gap column=（1.5~3）× stainless steel
The thickness of plate, thickness are the rectangular slabs of 0.5mm, are bent several foldings in the length direction of rectangular slab, bending angle is 100 ~ 120
Degree；Curved edges are contacted with faying face.
The magnesium alloy plate includes AZ31B magnesium alloy plates；
The stainless steel plate includes 2205,316L, 304 stainless steel plates；
The sheet copper includes T2 copper plates；
The length and width size of the magnesium alloy plate is respectively less than stainless steel plate 50mm；
The length and width size of the magnesium alloy plate is respectively less than sheet copper plate 50mm；
The sheet copper and stainless steel plate are equal in magnitude；
The explosive uses bulking ammonium nitrate explosive（Ammonium nitrate 85%, diesel oil 3%, sawdust 8.5%, industrial salt 3.5%）, density
0.85g/cm3,2500 ~ 2700m/s of detonation velocity.
Compared with prior art, the present invention having following apparent technical advances：
（1）Stainless steel double can be effectively improved the characteristics of Mg alloy surface is easily corroded on magnesium alloy, and simultaneously synthesizing answers
Plywood intensity is higher than magnesium alloy substrate.
（2）Layers of copper is added as transition zone, realizes indissoluble on metallurgy, the stainless steel and magnesium alloy that fusing point differs greatly are high
Effect connection.Transition zone generates metallurgical binding respectively with stainless steel, magnesium alloy, and then improves composite plate interfacial bonding strength.
（3）Using explosive welding production magnesium steel composite board for rolling is processed, advantage is, base compound plate area,
Thickness is unrestricted, the board size of composite plate made of explosive welding, and thickness can configure the combination of two kinds of base materials as needed
Ratio.Not by equipment limit, manufacturing cost is low.The disposable explosive forming of three ply board, it is easy to operate.
（4）Annealing patent is carried out to magnesium alloy plate before explosion, prevents blast process magnesium alloy embrittlement.
（5）It is buffered using rubber air mattress, prevents the magnesium alloy plate that ground recoil strength causes plasticity difference from cracking.
（6）Using the welding procedure of not uniform thickness cloth medicine, reduce the size in the non-soldering region in composite plate edge.
（7）The defects of microstructure observation's interface pore-free, crackle, interface cohesion is secured, and interface tensile-sbear strength 165 ~
183Mpa。
Description of the drawings
Fig. 1 is stainless steel-copper-magnesium alloy composite board explosion welding apparatus schematic diagram；
In figure：1, earthen foundation, 2, rubber base plate, 3 magnesium alloy plates, 4 first lamellar spacing columns, 5, copper plate, 6 second interlayers
Gap column, 7, stainless steel plate, 8, butter, 9, medicine frame, 10, nitrolite, 11, electric cap.
Fig. 2 is explosive welding stainless steel-copper-magnesium alloy composite board interface microscopic appearance；
In figure:A, stainless steel layer, B, layers of copper, C, magnesium alloy layer；
Fig. 3 is stainless steel-copper-magnesium alloy composite board interface location iron, copper line scanning figure；
Fig. 4 is stainless steel-copper-magnesium alloy composite board interface location copper, magnesium elements line scanning figure；
Fig. 5 is the shape graph of the curved edges of intermediate gap column of the present invention.
Specific implementation mode 1
（1）Select the base material of AZ31B magnesium alloy plates and 2205 stainless steel plates as explosive welding；T2 copper plates are as transition
Layer.
The specification of AZ31B magnesium alloy plates is 1050mmX600mmX3mm；
The specification of T2 copper plates is 1100 mmX650mmX0.5mm；
The specification of 2205 stainless steel plates is 1100 mmX650mmX2mm;
Before explosive welding, AZ31B magnesium alloy plates annealing toughening, 300 DEG C of annealing temperature, soaking time 120min.
（2）Using the method for mechanical grinding, the oxide layer and impurity at three kinds of material interfaces to be combined are removed；
Magnesium alloy plate and stainless steel plate face to be combined, using installation grinding wheel, wire brush angle grinder by stainless steel plate and
Magnesium alloy plate interface to be combined is just polished, and is then polished with the sand paper essence of 600 mesh, and surface roughness Ra to be combined is made to be no more than 2 μm.
Copper plate upper and lower surface is directly polished with 600 mesh sand paper, and surface roughness is no more than 2 μm.After polishing, prepare
Implement explosive welding.
（3）By the stainless steel plate handled well, copper plate and magnesium alloy board group to carrying out explosive welding；
（4）Explosive welding carries out on soil property ground, without other objects in the radius of 30 meters of periphery, is placed on soil
The cushion rubber layer of 2000mm X2000mmX5mm, cushion rubber layer are fixed with ground, after buffer layer is used for reducing explosion generation,
Ground is in face of the upward impact force of composite plate.Substrate magnesium alloy plate is placed on the buffer layer；
（5）Copper gap column is placed on magnesium alloy plate face to be combined, the spacing between the column of gap is 100mm, gap
Column uses copper foil, and gap column length 20mm, thickness is 0.5mm, and height is 4mm, and gap column is vertical with magnesium alloy plate holding；
（6）Copper plate is placed on the column of gap, copper plate is parallel with magnesium alloy plate, and copper is placed above in copper plate
Gap column, the spacing between the column of gap are 100mm, and gap column uses copper foil, and gap column length 20mm, thickness is 0.5mm, and height is 4mm,
Gap column is vertical with copper plate holding；
（7）Cladding corrosion resistant plate, stainless steel plate and substrate-parallel is placed above in copper plate；
（8）The side coating butter of surface and surrounding is as buffer layer, coating butter thickness on stainless steel
2mm；
（9）Brown paper medicine frame and butter are bonded.
（10）Expanded ammonium nitrate composite explosives are layered on not equal thickness above butter, are laid with from initiation ends to explosion end
Explosive thickness gradually successively decreases, and initiation ends explosive thickness is 40mm, and explosion ending end explosive thickness is 30mm；Explosive layer is from initiation ends
It is seamlessly transitted to explosion end；
（11）Detonator is mounted on initiation ends explosive edge, it is 25mm that detonator, which is inserted into explosive depth, 5 around detonator ~
5 ~ 8mg hexogen is uniformly added in 10mm radius；Detonator lead is more than outside 40 meters.
（12）A long way off, using trigger detonating primer, high energy impact that explosive generates from compound plate be transmitted to transition zone to
Substrate, instantaneous explosion welding are completed.
Explosive uses bulking ammonium nitrate explosive（Ammonium nitrate 85%, diesel oil 3%, sawdust 8.5%, industrial salt 3.5%）, density
0.85g/cm3,2500 ~ 2700m/s of detonation velocity.
（13）Stainless steel-copper-magnesium alloy three-layer composite board of explosion synthesis is annealed；It is multiple after elimination explosive welding
Plywood residual stress is made annealing treatment in resistance heating case, and 200 DEG C of annealing temperature is warming up to 10 DEG C of speed per second,
Soaking time 60min；After heat preservation, composite plate furnace cooling；
（14）It is smoothed on level(l)ing machine；
（15）The non-soldering region of composite plate surrounding is cut with plate shearing machine, the remaining butter in stainless steel plate upper surface of polishing obtains
To stainless steel-copper-magnesium alloy three-layer composite board；
（16）It detects a flaw to composite plate according to the requirement of GB/T 7734-2015 composite plate ultrasonic inspections, result of detection
Show composite plate Percentage bound 99.8%；
（17）According to GB/T6369-2008, test compound board interface tensile-sbear strength, the tensile-sbear strength at interface is
180.0Mpa carries out Surface scan analysis to tensile-shear crack interface, finds all copper of component of two planes of disruption, illustrates to draw and cut
Fracture illustrates interface bond strength height along copper transition fault rupture；
（18）Combination interface is observed using surface sweeping Electronic Speculum SEM, the defects of interface cohesion is intact, pore-free, crackle；
（19）Line surface sweeping analysis is done near interface using EDS, between magnesium elements and copper, copper and ferro element mutually
It mutually spreads, illustrates that two kinds of materials realize metallurgical binding by diffusion reaction.
Specific implementation mode 2
（1）Select the base material of AZ31B magnesium alloy plates and 316L stainless steel plates as explosive welding；T2 copper plates are as transition
Layer.
The specification of AZ31B magnesium alloy plates is 650mmX450mmX8mm；
The specification of T2 copper plates is 700mmX500mmX0.5mm；
The specification of 316L stainless steel plates is 700mmX500mmX2mm；
Before explosive welding, AZ31B magnesium alloy plates annealing toughening, 300 DEG C of annealing temperature, soaking time 120min.
（2）Using the method for mechanical grinding, the oxide layer and impurity at three kinds of material interfaces to be combined are removed；
Magnesium alloy plate and stainless steel plate face to be combined, using installation grinding wheel, wire brush angle grinder by stainless steel plate and
Magnesium alloy plate interface to be combined is just polished, and is then polished with the sand paper essence of 600 mesh, and surface roughness Ra to be combined is made to be no more than 2 μm.
Copper plate upper and lower surface is directly polished with 600 mesh sand paper, and surface roughness is no more than 2 μm.After polishing, prepare
Implement explosive welding.
（3）By the stainless steel plate handled well, copper plate and magnesium alloy board group to carrying out explosive welding；
（4）Explosive welding carries out on soil property ground, without other objects in the radius of 30 meters of periphery, is placed on soil
The cushion rubber layer of 2000mm X2000mmX5mm, cushion rubber layer are fixed with ground, after buffer layer is used for reducing explosion generation,
Ground is in face of the upward impact force of composite plate.Substrate magnesium alloy plate is placed on the buffer layer；
（5）Copper gap column is placed on magnesium alloy plate face to be combined, the spacing between the column of gap is 100mm, gap
Column uses copper foil, and gap column length 20mm, thickness is 0.5mm, and height is 4mm, and gap column is vertical with magnesium alloy plate holding；
（6）Transition zone copper plate is placed on the column of gap, copper plate is parallel with magnesium alloy plate, is placed above in copper plate
Copper gap column, the spacing between the column of gap are 100mm, and gap column uses copper foil, and gap column length 20mm, thickness is 0.5mm, high
It is 4mm, gap column is vertical with copper plate holding；
（7）Cladding corrosion resistant plate, stainless steel plate and substrate-parallel is placed above in copper plate；
（8）The side coating butter of surface and surrounding is as buffer layer, coating butter thickness on stainless steel
2mm；
（9）Brown paper medicine frame and butter are bonded.
（10）Expanded ammonium nitrate composite explosives are layered on not equal thickness above butter, are laid with from initiation ends to explosion end
Explosive thickness gradually successively decreases, and initiation ends explosive thickness is 40mm, and explosion ending end explosive thickness is 30mm；Explosive layer is from initiation ends
It is seamlessly transitted to explosion end；
（11）Detonator is mounted on initiation ends explosive edge, it is 25mm that detonator, which is inserted into explosive depth, 5 around detonator ~
5 ~ 8mg hexogen is uniformly added in 10mm radius；Detonator lead is more than outside 40 meters.
（12）A long way off, using trigger detonating primer, high energy impact that explosive generates from compound plate be transmitted to transition zone to
Substrate, instantaneous explosion welding are completed.
Explosive uses bulking ammonium nitrate explosive（Ammonium nitrate 85%, diesel oil 3%, sawdust 8.5%, industrial salt 3.5%）, density
0.85g/cm3,2500 ~ 2700m/s of detonation velocity.
（13）Stainless steel-copper-magnesium alloy three-layer composite board of explosion synthesis is annealed；It is multiple after elimination explosive welding
Plywood residual stress is made annealing treatment in resistance heating case, and 200 DEG C of annealing temperature is warming up to 10 DEG C of speed per second,
Soaking time 60min；After heat preservation, composite plate furnace cooling；
（14）It is smoothed on level(l)ing machine；
（15）The non-soldering region of composite plate surrounding is cut with plate shearing machine, the remaining butter in stainless steel plate upper surface of polishing obtains
To stainless steel-copper-magnesium alloy three-layer composite board；
（16）It detects a flaw to composite plate according to the requirement of GB/T 7734-2015 composite plate ultrasonic inspections, result of detection
Show composite plate Percentage bound 99.8%；
（17）According to GB/T6369-2008, test compound board interface tensile-sbear strength, the tensile-sbear strength at interface is
165.0Mpa carries out Surface scan analysis to tensile-shear crack interface, finds all copper of component of two planes of disruption, illustrates to draw and cut
Fracture illustrates interface bond strength height along copper transition fault rupture；
（18）Combination interface is observed using surface sweeping Electronic Speculum SEM, the defects of interface cohesion is intact, pore-free, crackle；
（19）Line surface sweeping analysis is done near interface using EDS, between magnesium elements and copper, copper and ferro element mutually
It mutually spreads, illustrates that two kinds of materials realize metallurgical binding by diffusion reaction.
Specific implementation mode 3
（1）Select the base material of AZ31B magnesium alloy plates and 304 stainless steel plates as explosive welding；T2 copper plates are as transition
Layer.
The specification of AZ31B magnesium alloy plates is 700mmX450mmX8mm；
The specification of T2 copper plates is 750mmX500mmX1mm；
The specification of 304 stainless steel plates is 750mmX500mmX3mm；
Before explosive welding, AZ31B magnesium alloy plates annealing toughening, 300 DEG C of annealing temperature, soaking time 120min.
（2）Using the method for mechanical grinding, the oxide layer and impurity at three kinds of material interfaces to be combined are removed；
Magnesium alloy plate and stainless steel plate face to be combined, using installation grinding wheel, wire brush angle grinder by stainless steel plate and
Magnesium alloy plate interface to be combined is just polished, and is then polished with the sand paper essence of 600 mesh, and surface roughness Ra to be combined is made to be no more than 2 μm.
Copper plate upper and lower surface is directly polished with 600 mesh sand paper, and surface roughness is no more than 2 μm.After polishing, prepare
Implement explosive welding.
（3）By the stainless steel plate handled well, copper plate and magnesium alloy board group to carrying out explosive welding；
（4）Explosive welding carries out on soil property ground, without other objects in the radius of 30 meters of periphery, is placed on soil
The cushion rubber layer of 2000mm X2000mmX5mm, cushion rubber layer are fixed with ground, after buffer layer is used for reducing explosion generation,
Ground is in face of the upward impact force of composite plate.Substrate magnesium alloy plate is placed on the buffer layer；
（5）Copper gap column is placed on magnesium alloy plate face to be combined, the spacing between the column of gap is 100mm, gap
Column uses copper foil, and gap column length 20mm, thickness is 0.5mm, and height is 5mm, and gap column is vertical with magnesium alloy plate holding；
（6）Transition zone copper plate is placed on the column of gap, copper plate is parallel with magnesium alloy plate, is placed above in copper plate
Copper gap column, the spacing between the column of gap are 100mm, and gap column uses copper foil, and gap column length 20mm, thickness is 0.5mm, high
It is 4mm, gap column is vertical with copper plate holding；
（7）Cladding corrosion resistant plate, stainless steel plate and substrate-parallel is placed above in copper plate；
（8）The side coating butter of surface and surrounding is as buffer layer, coating butter thickness on stainless steel
2mm；
（9）Brown paper medicine frame and butter are bonded.
（10）Expanded ammonium nitrate composite explosives are layered on not equal thickness above butter, are laid with from initiation ends to explosion end
Explosive thickness gradually successively decreases, and initiation ends explosive thickness is 45mm, and explosion ending end explosive thickness is 30mm；Explosive layer is from initiation ends
It is seamlessly transitted to explosion end；
（11）Detonator is mounted on initiation ends explosive edge, it is 30mm that detonator, which is inserted into explosive depth, 5 around detonator ~
5 ~ 8mg hexogen is uniformly added in 10mm radius；Detonator lead is more than outside 40 meters.
（12）A long way off, using trigger detonating primer, high energy impact that explosive generates from compound plate be transmitted to transition zone to
Substrate, instantaneous explosion welding are completed.
Explosive uses bulking ammonium nitrate explosive（Ammonium nitrate 85%, diesel oil 3%, sawdust 8.5%, industrial salt 3.5%）, density
0.85g/cm3,2500 ~ 2700m/s of detonation velocity.
（13）Stainless steel-copper-magnesium alloy three-layer composite board of explosion synthesis is annealed；It is multiple after elimination explosive welding
Plywood residual stress is made annealing treatment in resistance heating case, and 200 DEG C of annealing temperature is warming up to 10 DEG C of speed per second,
Soaking time 60min；After heat preservation, composite plate furnace cooling；
（14）It is smoothed on level(l)ing machine；
（15）The non-soldering region of composite plate surrounding is cut with plate shearing machine, the remaining butter in stainless steel plate upper surface of polishing obtains
To stainless steel-copper-magnesium alloy three-layer composite board；
（16）It detects a flaw to composite plate according to the requirement of GB/T 7734-2015 composite plate ultrasonic inspections, result of detection
Show composite plate Percentage bound 99.8%；
（17）According to GB/T6369-2008, test compound board interface tensile-sbear strength, the tensile-sbear strength at interface is
183.0Mpa carries out Surface scan analysis to tensile-shear crack interface, finds all copper of component of two planes of disruption, illustrates to draw and cut
Fracture illustrates interface bond strength height along copper transition fault rupture；
（18）Combination interface is observed using surface sweeping Electronic Speculum SEM, the defects of interface cohesion is intact, pore-free, crackle；
（19）Line surface sweeping analysis is done near interface using EDS, between magnesium elements and copper, copper and ferro element mutually
It mutually spreads, illustrates that two kinds of materials realize metallurgical binding by diffusion reaction.
Gap column of the present invention is that a block length is 10mm, the height of width=copper gap column=（1.5~3）× stainless
The thickness of steel plate, thickness are the rectangular slabs of 0.5mm, are bent several foldings in the length direction of rectangular slab, bend to shown in Fig. 5
Curved edges, bending angle be 100 ~ 120 degree；Curved edges are contacted with faying face.
99.8% Surface bond rate of the present invention is the Percentage bound for removing edge and being not associated with behind region.
Claims (2)
1. a kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board, is cladding using stainless steel, magnesium alloy is
Base, sheet copper are transition zone, using expanded ammonium nitrate composite explosives as the explosion energy；It is characterized in that：Include the following steps：
（1）Select magnesium alloy plate and stainless steel plate as the base material of explosive welding, and to magnesium alloy annealing toughening, annealing temperature is
300 DEG C, soaking time 120min；
（2）Stainless steel and magnesium alloy plate interface to be combined just polish with angle grinder, then carry out essence with the sand paper of 600 mesh
Polishing makes surface roughness Ra to be combined be no more than 2 μm；Sheet copper upper and lower surface is polished with 600 mesh sand paper, makes following table on sheet copper
Surface roughness is no more than 2 μm；
（3）By stainless steel plate, sheet copper and the magnesium alloy board group after polishing to carrying out explosive welding：
Cushion rubber layer is fixed in face to I on the ground；
Magnesium alloy plate is placed on cushion rubber layer by II；
Copper gap column is vertically disposed in above magnesium alloy plate by III, the spacing between copper gap column be 100mm, copper
Gap pillar height degree is（1.5~3）The thickness of × stainless steel plate；
Sheet copper is placed on copper gap column by IV, and sheet copper is parallel with magnesium alloy plate；
Copper gap column is placed above in sheet copper in V, and the spacing between copper gap column is 100mm, copper gap pillar height degree
For（1.5~3）The thickness of × stainless steel plate, copper gap column are vertical with sheet copper holding；
VI places stainless steel plate on sheet copper, and stainless steel plate is parallel with magnesium alloy plate；
The VII butter that the uniform smearing thickness of layer surface and edge is 2mm on stainless steel；
VIII bonds brown paper medicine frame with stainless steel plate edge with butter；
Uniform thickness is not laid with one layer of explosive above IV butter, and initiation ends explosive thickness is more than explosion ending end explosive thickness；Explosive
Layer is seamlessly transitted from initiation ends to explosion ending end；
Detonator is inserted into explosive layer by X, be inserted into explosive layer cap length be more than initiation ends explosive thickness half, and
5 ~ 8mg hexogen is added around detonator in 5 ~ 10mm radius；
（4）Stainless steel-copper-magnesium alloy three-layer composite board of explosion synthesis is made annealing treatment, is heated up with 10 DEG C/sec of speed
To 200 DEG C, soaking time 60min of annealing temperature, after heat preservation, then composite plate furnace cooling is smoothed on level(l)ing machine；
（5）The non-soldering region of composite plate surrounding is cut with plate shearing machine, the remaining butter of stainless steel upper surface side of polishing obtains stainless
Steel-copper-magnesium alloy three-layer composite board；
（6）The Percentage bound of stainless steel-copper-magnesium alloy three-layer composite board is 99.8%, and tensile-sbear strength is 165 ~ 183Mpa, magnesium elements
It spreads mutually between copper, is spread mutually between copper and ferro element；
The copper gap column is that a block length is 20mm, width=（1.5~3）The thickness of × stainless steel plate, thickness are 0.5mm
Rectangular sheet is bent several foldings in the length direction of rectangular sheet, and bending angle is 100 ~ 120 degree；Curved edges and faying face
Contact.
2. a kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board, feature exist according to claim 1
In：Magnesium alloy plate is AZ31B magnesium alloy plates, and stainless steel plate is 2205 stainless steel plates；The specification of AZ31B magnesium alloy plates is
1050mmX600mmX3mm；The specification of sheet copper is 1100 mmX650mmX0.5mm；The specification of 2205 stainless steel plates is 1100
mmX650mmX2mm。
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710052452.8A CN106624330B (en) | 2017-01-24 | 2017-01-24 | A kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710052452.8A CN106624330B (en) | 2017-01-24 | 2017-01-24 | A kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106624330A CN106624330A (en) | 2017-05-10 |
| CN106624330B true CN106624330B (en) | 2018-09-18 |
Family
ID=58841224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710052452.8A Active CN106624330B (en) | 2017-01-24 | 2017-01-24 | A kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106624330B (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107009017A (en) * | 2017-05-15 | 2017-08-04 | 湖北金兰特种金属材料有限公司 | A kind of complex method of three-layer metal material single explosive forming |
| CN107553060A (en) * | 2017-08-24 | 2018-01-09 | 洛阳双瑞金属复合材料有限公司 | A kind of manufacture method of copper rustless steel double-metal composite contact matrix material |
| CN108788439B (en) * | 2018-06-15 | 2021-01-29 | 中国矿业大学 | Explosive welding method for lead-zinc stainless steel multilayer radiation-proof composite board |
| CN109457263B (en) * | 2019-01-02 | 2021-02-23 | 吉林大学 | Method for preparing magnesium alloy-stainless steel composite board |
| CN109894734A (en) * | 2019-04-10 | 2019-06-18 | 南京昭邦金属复合材料有限公司 | Super thick degree is than stainless steel-copper composite plate explosion welding method |
| CN112719558B (en) * | 2020-12-22 | 2021-12-28 | 中国科学技术大学 | Energy control method for multilayer explosive welding |
| CN112846650A (en) * | 2020-12-25 | 2021-05-28 | 河北万丰冶金备件有限公司 | Method for manufacturing cooling wall of blast furnace |
| CN113478064A (en) * | 2021-07-20 | 2021-10-08 | 西安天力金属复合材料股份有限公司 | Explosive welding method for copper-aluminum-copper three-layer composite board |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007015018A (en) * | 2005-06-08 | 2007-01-25 | Asahi Kasei Chemicals Corp | Magnesium composite material and its manufacturing method |
| CN102430900A (en) * | 2011-10-30 | 2012-05-02 | 太原钢铁(集团)有限公司 | Composite steel plate and manufacturing method thereof |
| CN103586574A (en) * | 2013-10-16 | 2014-02-19 | 太原理工大学 | Explosive welding forming method of magnesium and aluminum alloy composite plates |
| CN104526151A (en) * | 2014-12-02 | 2015-04-22 | 太原理工大学 | Explosive welding forming method for magnesia-alumina-titanium alloy composite board |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6572984B2 (en) * | 2001-04-17 | 2003-06-03 | Intriplex Technologies, Inc. | Metal laminate structure and method for making |
-
2017
- 2017-01-24 CN CN201710052452.8A patent/CN106624330B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007015018A (en) * | 2005-06-08 | 2007-01-25 | Asahi Kasei Chemicals Corp | Magnesium composite material and its manufacturing method |
| CN102430900A (en) * | 2011-10-30 | 2012-05-02 | 太原钢铁(集团)有限公司 | Composite steel plate and manufacturing method thereof |
| CN103586574A (en) * | 2013-10-16 | 2014-02-19 | 太原理工大学 | Explosive welding forming method of magnesium and aluminum alloy composite plates |
| CN104526151A (en) * | 2014-12-02 | 2015-04-22 | 太原理工大学 | Explosive welding forming method for magnesia-alumina-titanium alloy composite board |
Non-Patent Citations (1)
| Title |
|---|
| Microstructural characteristics of joint region during diffusion-brazing of magnesium alloy and stainless steel using pure copper interlayer;Xin-jian YUAN et al;《Transactions of Nonferrous Metals Society of China》;20131231(第3期);第599-604页 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106624330A (en) | 2017-05-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106624330B (en) | A kind of explosive welding processing method of stainless steel-copper-magnesium alloy composite board | |
| CN106825898B (en) | A kind of explosive welding processing method of stainless steel magnesium alloy composite board | |
| CN105478475B (en) | A kind of method of rolling high-strength degree composite metal plate | |
| CN101352805B (en) | Method for producing stainless steel composite steel plate | |
| Li et al. | Interfacial microstructure and mechanical properties of dissimilar aluminum/steel joint fabricated via refilled friction stir spot welding | |
| CN110421000B (en) | Method for preparing metal composite plate by cross rolling of double corrugated rollers | |
| CN103586574B (en) | A kind of explosive welding forming method of magnadure composite plate | |
| CN108326516B (en) | Preparation method of titanium steel composite board | |
| CN103286434B (en) | A kind of high-strength laminated composite plate preparation method | |
| CN102581006B (en) | Hot-rolling compounding method for titanium/aluminum/titanium three-layer composite plate | |
| Fernandus et al. | Developing Temperature–Time and Pressure–Time diagrams for diffusion bonding AZ80 magnesium and AA6061 aluminium alloys | |
| CN101402268A (en) | Titanium and titanium alloy/steel composite board and method of manufacturing the same | |
| CN105478476B (en) | A kind of method of rolled metal complex plate strip | |
| CN102240845A (en) | Explosive welding process for super-long and super-wide composite boards | |
| RU2560472C2 (en) | Making of sandwiched material | |
| CN104862454B (en) | A kind of high hardness material surface treatment method and device | |
| CN106271017A (en) | A kind of explosion welding method of aluminium alloy fine aluminium steel composite board | |
| CN109693430A (en) | Thin-clad double-sided titanium steel composite plate and preparation method thereof | |
| Ao et al. | Microstructure and mechanical properties of dissimilar NiTi and 304 stainless steel joints produced by ultrasonic welding | |
| CN108340129A (en) | A kind of preparation method of the stainless steel and carbon steel composite tube on the deposited side of easy welding | |
| CN114192580A (en) | Preparation method of cross corrugated interface metal composite plate | |
| CN105728492A (en) | Clad steel plate with yield strength larger than 700 MPa and manufacturing method of clad steel plate | |
| CN110216364B (en) | Ultrasonic consolidation forming method for zirconium steel layered composite material | |
| CN114131159A (en) | Welding method of ultrahigh-strength steel Q1300E steel plate | |
| CN206456036U (en) | Titanium al stainless steel multilayer overlarge area explosive clad plate |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221102 Address after: No. 10, Electronic Street, Tanghuai Industrial Park, Shanxi Transformation Comprehensive Reform Demonstration Zone, Taiyuan, Shanxi Province, 030000 Patentee after: SHANXI YANGMEI CHEMICAL MACHINERY (GROUP) Co.,Ltd. Address before: 030024 Shanxi province Taiyuan city Berlin District Wan wa flow Road No. 66 Patentee before: TAIYUAN University OF SCIENCE AND TECHNOLOGY |
|
| TR01 | Transfer of patent right |